June 5, 2013 at 4:03 pm
Hi all,
Hope somebody can help (and that I am posting in the right place).
Basically I am doing some research at university into increase in fuel burn per kg additional weight carried per flight. I have some catch-all figures that I have found on line but nothing that shows how such figures have come about.
I have found little so far to help me with this in the way of forumla but as I understand it fuel use will be some sort of combination aircraft type, distance, pax (and pax weight), Cargo, empty mass, fuel carried, fuel not burned. I am not sure however of how these figures can be put together to show how fuel use will reduce with an increase in weight though!
I am also wondering where I can get the data I need. I understand that I will have to use a number of assumptions (actual pax / pax weight / cargo), and I’m sure I can dig out that sort of stuff from somewhere, however not sure where I can get info on flight distance / aircraft type, or not without going through each departure one by one anyway!
Any help or advice gratefully appreciated. If I have been too vague in areas or confusing please let me know but be nice 🙂
Thanks,
Marty
Additional;
– For the study I am looking at all flights leaving Manchester and Heathrow on a given day.
By: Amiga500 - 6th June 2013 at 20:30
I have found little so far to help me with this in the way of forumla but as I understand it fuel use will be some sort of combination aircraft type, distance, pax (and pax weight), Cargo, empty mass, fuel carried, fuel not burned. I am not sure however of how these figures can be put together to show how fuel use will reduce with an increase in weight though!
Start from engine efficiency and build it back up. The propulsive efficiency of an engine might be around 0.70. The thermal efficiency might get up toward 0.5, giving overall engine efficiency of 0.35 or so.
Figure out your aircraft L/D for various stages of flight (well, estimate it). You know the energy content of fuel. Decide your payload weight. Add in your divert fuel and you have your end-mission weight. Therefore you know the required fuel consumption at the end of flight.
Work backwards towards the start of the flight (mission length is up to you), accumulating the fuel needed to finish the flight which will add to your lift dependent drag.
The Breguet range equation may be useful for the cruise portion of flight.